View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 17296U 87003B 25197.93153200 .00000352 00000-0 38022-4 0 9999
2 17296 82.5303 142.3613 0017563 198.8145 161.2424 14.85319553 59701
| Epoch (UTC): | 16 July 2025 22:21:24 |
| Eccentricity: | 0.0017563 |
| inclination: | 82.5303° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 142.3613° |
| argument of perigee: | 198.8145° |
| revolutions per day: | 14.85319553 |
| mean anomaly at epoch: | 161.2424° |
| orbit number at epoch: | 5970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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